▸Orbital parameters

Orbit class	SSO
Inclination	97.5052°
Eccentricity	0.0009042
Period	94.3 min
Apogee	491 km
Perigee	478 km
Mean motion	15.27087980 rev/day
RAAN	251.8545°
Arg of perigee	32.4196°
Mean anomaly	327.7597°
B*	2.5376e-4
Rev at epoch	16,736

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 57188U 23091Y 26188.16399560 .00006675 00000-0 25376-3 0 9998

2 57188 97.5052 251.8545 0009042 32.4196 327.7597 15.27087980167369

▸ source OMM (JSON)

{
  "OBJECT_NAME": "HORS 1",
  "OBJECT_ID": "2023-091Y",
  "EPOCH": "2026-07-07T03:56:09.22+00:00",
  "MEAN_MOTION": 15.2708798,
  "ECCENTRICITY": 0.0009042,
  "INCLINATION": 97.5052,
  "RA_OF_ASC_NODE": 251.8545,
  "ARG_OF_PERICENTER": 32.4196,
  "MEAN_ANOMALY": 327.7597,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 57188,
  "REV_AT_EPOCH": 16736,
  "BSTAR": 0.00025376,
  "MEAN_MOTION_DOT": 0.00006675,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	HORS 1
Operator	Baumann Moscow State Technical UniversityHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Jun 27, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/57188

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.